View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40069U 14037A 23091.15621867 .00000111 00000-0 70500-4 0 9994
2 40069 98.4259 100.7008 0005211 194.7465 165.3567 14.20761000452712
Epoch (UTC): | 01 April 2023 03:44:57 |
Eccentricity: | 0.0005211 |
inclination: | 98.4259° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 100.7008° |
argument of perigee: | 194.7465° |
revolutions per day: | 14.20761000 |
mean anomaly at epoch: | 165.3567° |
orbit number at epoch: | 45271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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